MACH 3.5 Boundary-Layer Transition on a Cone at Angle of Attack
22nd Fluid Dynamics, Plasma Dynamics and Lasers Conference ; 1991 ; Honolulu , HI , U.S.A.
01.01.1991
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Hypersonic Boundary Layer Transition on a 7 Degree Half-Angle Cone at Mach 10
British Library Conference Proceedings | 2014
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